Monday, December 5, 2016

Private Pilot Course - Ground Portion - Oral Exam


Private Pilot Course - Ground Portion - Oral Exam


  • Knowledge Exam  - Computerized Exam
  • Oral Exam  - With Examination
  • Practical Exam  - Fly the Flight Plan, Diversion, Maneuvers, Under hood


Required Documents
  • Student Pilot Certificate
  • Medical Certificate
  • Government Issued Photo ID
  • Log Book
  • Knowledge Test Results
Examiner Verify Sec 61.109 is met    (use sticker to highlight section)
- Hours
- Takeoffs
- Landings
- Flight Distances Required

Instructor Endorsements in Logbook Verify Sec 61.107 and Verify Sec 61.105

ICARA   Integrated Airman Certification and Rating Application (On Line)
Pilot's Bill of Rights, Electronic Sign . Validate ID.

1. Plan A VFR Flight, Fuel, Weight and Balance

2. Airplane  
ARROW (Airworthiness, Registration, Radio, Operating Limits, Weight and Balance)
Engine / Airplane Logs
Inspection -
Last 100 hours inspection
Transponder Test
ELT Battery
ELT 12 months inspection
Registration

Mark with TABS -

AD Note - FAA Airworthiness Directive   Recurring  done in log in log book
Annual Inspection  - Airplane logbook / Airframe Log book

To take passenger 3 take off and landing within 90 days
1 every 24 calendar month

Night - 3 take off and landing with 90 days to a full stop
sunset and sun

3. Weather for the Flight -
Forecast of destination airport  - Terminal Area Forecast
Winds Alof on Flight path  3,000'  6,000  Temperature /Winds
Nodams - Notice to Airman  things out broken, closed
Weather Charts - Weather depiction -   Ares of IFR marginal VFR,
Radar Summary - Precipitation
Weather Prog Chart -  4 panel forecast  surface weather, weather to 24,000'

Sigmet - Signaficant - sever s
Airmet - lighter turbulence / freezing lev
Convective Signemt -

Windshare airport  - Use Higher indicator airspeed

4. POH -
Use of Charts - Take off distance problem (performance Section)
Gross weight  - Lift off speed / higher pressure altitude (altitude at standard 29.92)  elevation and temperature (use warmer temperature)   Ground roll  50' Obstacle

Cruse Performance   - 70% Power True Airspeed / fuel consumption GPH

Temperature At 8,000'  True Airspeed 140 Knots True .. Calibrated Airspeed
Head Wind/Tail Wind component

Landing Distance Problem -
23:00mins

Higher Distance Altitude - Use of Flaps  

Density altitude is pressure altitude corrected by non standard temperature -
The higher the density altitude the worst the aircraft will perform
Temperature 90 deg outside  6,100'  29.93    -  densitity altitude 10,000'   - aircraft will perform at 10,000 feet ...  poor performance


5. Weight and Balance
Moments arm CG  envelope

https://www.youtube.com/watch?v=kr483zBbQKw









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